Boeing 727-22

Service difficulty reports · 1,282

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '72722'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 97FDEA00131Chord · corrodedNR 0137 002, BULGE IN FLOOR WEB AT MID NOSE CHORD BS 298, LBL 15, WL 169. *S/D* REMOVED NOSE GEAR AND LT DOOR. REMOVED CENTER AND INBOARD L FLOOR WEB AND MID NOSE CHORD, DRILLED AND INSTALLED MID NOSE CHORD, FABRICATED WEB AND SPLICE PLATE. DRILLED AND INSFeb 27, 1997 · N148FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00169Frame · corrosion0332 005, WHILE WORKING CUSTOMER CARD 7-5330-7-2319G PT 3, FOUND CORROSION AT BS 360, WL 208, LBL 65 ON FRAME. *S/D* REMOVED DAMAGED FRAME AT BS 360, STR 13 LT TO 24 LT. FABRICATED NEW FRAME AND INSTALLED PER FED-EX SRM 53-10-4 FIGURE 3.Feb 26, 1997 · N148FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00120Frame · corrodedNR 0173 001, CORROSION (C53-113-01) IN FWD CARGO BAY BETWEEN FRAME AND REINFORCEMENT STRAP AT BS 580, LBL 32, WL 160. *S/D* CUTOUT DAMAGE FRAME, FABRICATED PART ALODINE, PRIMED AND INSTALLED REPAIR IAW FED-EX SRM 53-10-1 AND 51-40-3.Feb 21, 1997 · N148FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00134Channel · crackedNR 0106 004 FORWARD ENTRY DOOR UPPER HINGE CUTOUT H-CHANNEL IS CRACKED. REMOVED FORWARD ENTRY DOOR UPPER HINGE H-CHANNEL AND INSTALLED NEW H-CHANNEL IN SAME LOCATION PER FED-EX SRM 51-30-5, 51-30-2.Feb 17, 1997 · N148FE · Boeing 72722 · Passenger/Crew DoorsSDR CA970114005Bolts · corroded(CAN) DURING SKIN PANEL REPLACEMENT IN AREA STRINGER END FITTING TIE BOLTS WERE REMOVED TO ACCESS FASTENERS THROUGH BS1183 FRAME FLANGE. TIE BOLT SHANKS CORRODED, FROM LIGHT TO SEVERE CORROSION. CORROSION NOT DETECTABLE WITH BOLTS INSTALLED. BOLTS REPLACED.Dec 21, 1996 · Boeing 72722 · Fuselage Miscellaneous StructureSDR CA970114004Skin · cracked(CAN) CRACK INDICATION IN FUSELAGE PRESSURIZATION SKIN AT BS1170 ABOVE STRINGER 18L. CRACK THREE INCHES IN LENGTH JOINED A HORIZONTAL LINE OF PAINT BLISTERS IN A 10 INCH LINE OF BLISTERS. DISBONDED DOUBLER AND SEVERE CORROSION OF SKIN AND DOUBLER ON BOND FACESDec 17, 1996 · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA01694Switch Spacer · missingNR 2 LEADING EDGE FLAP FAILED TO RETRACT AFTER TAKEOFF. FOLLOWED CHECKLIST WITH NO RESULTS, RETURNED TO PORTLAND. REMOVED AND REPLACED NR 2 FLAP SWITCH, FOUND SPACER MISSING. INSTALLED SPACER, OPERATIONAL CHECK SEVERAL TIMES OPERATIONAL CHECK GOOD PER MAINTNov 27, 1996 · N168FE · Boeing 72722 · Leading Edge Slat Control SystemSDR DHL96707004Inlet Bullet · malfunctionedREJECTED TO NR 3 ENGINE, NOT MAKING TARGET EPR WITH ENGINE A/I ON. PARAMETERS ON ENGINE NR 1 WERE EPR 2.00 NI 96 PERCENT EGT 520 N2 93.5 F/F 9,500. ENGINE NR 3 PARAMETER WERE EPR 1.86 WITH A/I OFF NR 1 AND NR 3 ENGINE NORMAL. REMOVED AND REPLACED NR 3 ENGINNov 21, 1996 · N707DH · Boeing 72722 · Turbine Engine Air Inlet SectionSDR 96FDEA01656Gcu · water contamNR 1 GENERATOR TRIPPED OFF LINE 2-3 MINUTES AFTER TAKEOFF. BUS TIE WOULD NOT CLOSE PER CHECKLIST. FINALLY DID CLOSE BUT FIELD WOULD THEN NOT CLOSE WITH GOOD RESIDUAL VOLTS. REMOVED AND CLEANED WATER FROM GCU. REINSTALLED, OPS CHECKED NORMAL PER JRH 8-3.Nov 7, 1996 · N189FE · Boeing 72722 · AC RegulatorSDR 96FDEA01653Chord · corrodedNR 0041 002, CORROSION (C53-111-03 1/2) IN E-BAY DOGHOUSE ON VERTICAL CHORD AT BS 351 RBL 15 WL 169. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REMOVED VERTICAL CHORD, FABRICATED AND INSTALLED NEW VERTICAL CHORD AT BS 351, RBL 15, W/L 169 IAW FEDEX SRM 53-1Nov 5, 1996 · N149FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01652Chord · corrodedNR 0039 003, CORROSION ON BS 740 LOWER CHORD RBL 20 AND BLO. *S/D* SPLICED IN A NEW 740 LOWER CHORD IAW FEDEX EA 7-5710-31288.Nov 5, 1996 · N149FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01649I/B Aft Flap · delaminatedNR 0151 001 LT WING I/B AFT FLAP HAS TWO AREAS OF DELAMINATION IN O/B AFT HALF SECTION. REPAIRED DAMAGED SKIN TO LT WING I/B AFT FLAP IAW FEDEX SRM 51-40-6.Nov 4, 1996 · N149FE · Boeing 72722 · Wing, Control SurfacesSDR 96FDEA01629Bear Strap · corrodedNR 0108 003, CORROSION IN AFT CARGO BAY ON FWD SIDE OF FRAME ON INTERNAL SURFACE OF BEAR STRAP AT BS 1110 RLB 30 TO 45 WL 146 TO 156. *S/D* REPAIRED BEAR STRAP AT BS 1110 RBL 30 TO 45 WL 146 TO 156 IAW FEDEX EA 7-5330-31236.Oct 29, 1996 · N150FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01628Beam · corrodedNR 0253 002, WHILE WORKING CUSTOMER CARD NR 0172 FOUND CORROSION ON UPPER SURFACE OF L-ANGLE BS 740 WL 170 LBL 30 TO RBL 25. *S/D* REPAIRED L-ANGLE AT BS 740 WL 170 LBL 30 TO RBL 25 IAW FEDEX EZ 7-5310-31159.Oct 29, 1996 · N150FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01597Spar Chord · corrodedNR0172 - 001, CORROSION (C53-132-02-01) ON LOWER 740 CHORD AT LBL 4. *S/D* REMOVED CORRODED BS 740 FRONT SPAR LOWER CHORD AND INSTALLED NEW BS 740 FRONT SPAR LOWER CHORD PER FEDEX EA NR 7-5710-31160.Oct 20, 1996 · N150FE · Boeing 72722 · Wing SparSDR 96FDEA01554Nose Gear · malfunctionWHEN LANDING GEARS WERE EXTENDED ON APPROACH, THE MAINS EXTENDED GREEN, BUT THE NOSE GEAR LIGHT REMAINED AMBER. NO NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL. CYCLED GEAR AND ALL GEAR EXTENDED NORMALLY. PERFORMED NOSE GEAR EXTENSION AND RETRACTION TEST Sep 30, 1996 · N101FE · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR 96FDEA01550Hyd Line · crackedIN-FLIGHT AT FL 280, NR 1 ENGINE HYDRAULIC PUMP LIGHT STARTED BLINKING WITH FLUCTUATION IN PRESSURE. TWO SECONDS LATER, NR 2 ENGINE HYD PRESS LIGHT BLINKED, THEN BOTH LIGHTS CAME ON STEADY WITH RAPID LOSS OF ALL A-SYSTEM HYD FLUID. PUMPS WERE OPERATED WITHOUSep 26, 1996 · N107FE · Boeing 72722 · Hydraulic System, MainSDR 96FDEA01493Cable · dislodgedAFT CARGO DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL ILLUMINATED DURING CLIMBOUT PASSING 2,600 FEET. RETURN TO FIELD TO TROUBLESHOOT. FOUND CABLE STUCK IN DOOR JAMB. OPENED AND CLOSED DOOR, ALL LIGHTS WENT OUT.Sep 19, 1996 · N194FE · Boeing 72722 · Cargo/Baggage DoorsSDR 96FDEA01467Skin · corrodedFUSE SKIN BULGING AROUND FASTENERS STA 1163 STR 27 AND 26L. CUT OUT SKIN, REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-30-3.Sep 9, 1996 · N167FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA01469Skin · corrodedFUSELAGE EXT, SKIN BULGE AT STR 29L AFT OF STA 1080 FRAME. REMOVED CORROSION, INSTALLED FILLER AND DOUBLER PER SRM 53-30-3, SEALED EDGES OF DOUBLER PER SRM 51-20-04.Sep 4, 1996 · N167FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA01423Frame · crackedNR 0255 AND 037, CRACK ON FRAME AT BS 1110, STR 27R, RBL 22 WL 153.Sep 2, 1996 · N196FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA01420Skin · corrodedREMOVE AND INSTALLED NEW BELLY SKIN FROM BS 950 TO 1080.45, STR 26 LT TO 26 RT DUE TO MULTIPLE REPAIRS REQUIRED. REMOVED AND REPLACED BELLY SKIN FROM BS 950 TO 1080.45 STR 26 RT TO STR 26 LT IAW RED EX EA 7-5330-29745.Aug 30, 1996 · N196FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 96FDEA01418Web · corrosionWHILE WORKING NR O610, FOUND CORROSION ON WEB UNDER STIFFENER, STA 310, WL 184. REMOVED CORRODED WEB, FABRICATED NEW WEB AND SPLICE AT BS 294 TO BS 315, RBL 12 - LB 12, WL 184. REMOVED AND REPLACED 2 EACH CLIPS AT 294 - 301.5, RBL 12 AND LBL 12, WL 184 DAug 29, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01401Floor Beam · corrosionNR-0618 032, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 680 RBL 20 TO LBL 20 WL 200 FWD BAY.Aug 23, 1996 · N196FE · Boeing 72722 · Fuselage Main, Floor BeamSDR DHL96707003Pressure Line · rupturedAFTER T/O AROUND 30 MIN OUT OF IAH, AIRCRAFT SUFFERED COMPLETE FAILURE OF HYDRAULIC A-SYSTEM. TURNED BACK TO IAH. AIRCRAFT LANDED AND STOPPED AT END OF RUNWAY WAITING TO BE TOWED. RAMP FOUND NOSE GEAR HOSE BROKEN. REPLACED HOSE WITH FLEX LINE, CHECKED BOTHAug 22, 1996 · N707DH · Boeing 72722 · Hydraulic System, MainSDR 96FDEA1395Stringer · corrodedNR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964.Aug 22, 1996 · N196FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA01395Stringer · corrodedNR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964. *S/D* REMOVED CORROSION ON SIR 30 BS 964, OUT OF LIMITS IAW FEDEX SRM 53-10-01. REPAIRED STRINGER IAW FEDEX SRM 53-10-03.Aug 22, 1996 · N196FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA01385Angle · corrodedNR0698 AND 029, CORROSION ON KEEL BEAM SUPPORT ANGLE AT BS 950 LBL TO RBL 5 WL 138.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01383Shear Tie · corrodedNR0673 AND 028, WHILE WORKING NR0668 FOUND BULGE IN BETWEEN SKIN AND FRAME AT BS 1030 BETWEEN STR 18 TO 19L.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01382Fitting · corrodedNR0360 AND 027, CORROSION (C57-581-01-1) LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IS CORRODED. *S/D* REMOVED AND REPLACED LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IAW FEDEX SRM 51-30-2.Aug 19, 1996 · N196FE · Boeing 72722 · Aileron Control SystemSDR 96FDEA01381Doubler · corrosionNR0696 AND 002, CORROSION ON SKIN SPLICE DOUBLER AT BS 1080 FROM RBL 23 TO LBL 32 WL 140. ALSO, (P/N 65-18387-15). *S/D* REMOVED CORROSION ON SKIN SPLICE DOUBLER AT BS 1080 RBL 23 TO LBL 32 WL 140, FOUND TO BE OUT OF LIMITS. REMOVED FABRICATED SKIN SPLICE Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01380Stringer · corrodedNR0129 AND 025, CORROSION (C53-224-02, -1) ON STR 6L BS 700 TO 680. *S/D* CORROSION ON STR NR 6L BS 700 TO 680 WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED STRINGER PER FEDEX SRM 53-10-3 FIG 3.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA01379Stringer · crackedNR0672 AND 024, WHILE WORKING NR201 FOUND STR TO BE CRACKED AT BS 1082 WL 138 STR 29L.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA01378Shear Tie · crackedNR0681 AND 023, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 29 TO 30R.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01377Shear Tie · crackedNR0682 AND 022, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 28 TO 29R. *S/D* REMOVED CRACKED SHEAR TIE AND REPLACED IAW FEDEX SRM 51-30-2.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01376Shear Tie · crackedNR0683 AND 021, CRACKED SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30R.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01375Shear Tie · corrodedNR0689 AND 020, CORROSION ON SHEAR TIE AT BS 170 BETWEEN STR 28 TO 29R.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01374Shear Tie · corrodedNR0690 AND 019, CORROSION ON SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30L. *S/D* REPAIRED SHEAR TIE AT BS 990 BETWEEN STRINGER 29 LEFT AND 30 LEFT AS PER FEDEX SRM 51-30-2.Aug 19, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01384Clip · crackedNR0119 AND 018, CRACKED STR CLIP AT BS 970 STR 16R. *S/D* REMOVED CRACKED STRINGER CLIP AT BS 970 STRINGER 16 RT AND REPLACED WITH NEW IAW FEDEX SRM 51-30-2.Aug 16, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01372Floor Beam · corrodedNR0550 AND 017, CORROSION (C53-224-01, -1) ON FLOOR BEAM UPPER CHORD BS 344 LBL 65 RBL 17 WL 208.Aug 16, 1996 · N196FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA01370Relay · dirtyCLIMBING OUT AT APPROX FLT LVL 250, HIGH PITCHED HOWL STARTED, FOLLOWED BY LOSS OF CABIN PRESS. UNABLE TO CONTROL CABIN PRESSURE USING BOTH PACKS. REMOVED AND REPLACED SAFETY RELAY, CLEANED AND OPS CK'D, OUTFLOW VALVES PER ENGINE RUN TO STEADY 4 PSI.Aug 15, 1996 · N187FE · Boeing 72722 · Cabin Pressure Control SystemSDR 96FDEA01367Former · corrodedNR 0664 AND 016. WHILE WORKING NR 0647, DISCOVERED CORROSION ON RT LOWER SKIN FORMER ANGLE AT BS 951, RBL 8 WL 138. ****S/D**** COMING.Aug 15, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01366Floor Beam · corrodedNR 0627 AND 015. CORROSION C53-224-01(1) AND BARE METAL ON BS 560 BEAM FROM LBL 62 - RBL 24 WL 208.1. ******S/D**** COMING.Aug 15, 1996 · N196FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 96FDEA01365Stiffener · corrosionNR 0611 AND 014. CORROSION C53-111-01 ON HORIZONTAL STIFFENER STA 310 RBL 12 WL 178. ****S/D****** COMING.Aug 14, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01364Stiffener · corrosionNR 0607 AND 013. CORROSION C53-111-01(1) ON HORIZONTAL STIFFENER STA 314 RBL 12 WL 178. ****S/D***** COMING.Aug 14, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01363Frame · corrodedNR 0623 AND 012. CORROSION C53-111-01 ON FRAME STA 700 STR 27L - R WL 156. ****S/D***** COMING.Aug 14, 1996 · N196FE · Boeing 72722 · Fuselage Main, FrameSDR 96FDEA01357Chord · corrodedNR0562 AND 011, CORROSION (C53-224-08) ON 1176.9 REINFORCEMENT CHORD AT LBL 63 WL 208.1 OUT OF LIMITS PER FEDEX SRM 53-10-01.Aug 13, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01356Keel Beam · corrodedNR0647 AND 010, CORROSION (C53-100-3) BETWEEN SKIN AND KEEL BEAM BS 1062 STR 29R. *S/D* REMOVED AND REPLACED RT KEEL BEAM STR 29R FROM BS 960 TO BS 1090 PER SB 727-53-0179.Aug 13, 1996 · N196FE · Boeing 72722 · Fuselage Main, KeelSDR 96FDEA01355Nose Chord · corrosionNR0610 AND 009, CORROSION (C53-111-01, -1) ON RT UPPER NOSE CHORD STA 312, 318, 330 RT WL 168 DOG HOUSE. *S/D* REMOVED AND REPLACED RT MID NOSE CHORD BS 294 TO 351 WL 169 RBL 15 AND REINSTALLED ALL ITEMS REMOVED FOR ACCESS.Aug 13, 1996 · N196FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 96FDEA01422Stringer · corrodedNR 0597 AND 036, BULGE IN SKIN AT BS 1157, STR 27 L.Aug 12, 1996 · N196FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
Back to Boeing 727-22